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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/45777

    Title: 小(微)衛星姿態控制分析與設計
    Other Titles: Attitude Control Analysis and Design for a Micro-Satellite
    Authors: 洪祖昌;Hong, Zuu-Chang;林煥榮;Lin, Huan-Rong;李大本;Lee, Da-Ban;陳正興;Chern, Jeng-Shing
    Contributors: 淡江大學航空太空工程學系
    Keywords: 微衛星;重力梯度;模糊控制;Micvosatellote;Gravity gradient;Fuzzy control
    Date: 1997-06
    Issue Date: 2013-03-20 16:22:46 (UTC+8)
    Publisher: 臺南市:中國航空太空學會
    Abstract: 本文主要目的是針對TUU SAT.1小微衛星的任務需求,且考慮衛星軌道、熱傳、太空環境、研製成本等因素的限制,決定採用重力梯度穩定被動控制方法配合主動的磁力矩控制方式,進行TUU SAT.1小微衛星的姿態控制設計,而控制器的原理採用模糊理論。
    In this paper, the attitude controller of TUU-SAT is designed, After we have considered these factors of orbit, thermal, Space environment and cost, the Passive Gravity Gradient Stabilization type is adopted, and where the magnetic-torquers produced magnetic field to affect the earth's magnetic field, then grow a magnetic force to correct the attitude of Satellite. The attitude controller is based on fuzzy logic control.
    Relation: 中國航空太空學會學刊=Transactions of the Aeronautical and Astronautical Society of the Republic of China 29(2),頁109-114
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

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